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Page 14 SPECIFICATION 80, ISSUE 1
4.6.8 Immersion
Specimens of sufficient length to perform the subsequent tests shall be measured at their
midpoints to determine their initial diameters, and shall then be immersed to within 6 inches
(152 mm) of their ends in each of the fluids (using a separate specimen for each fluid) for the
time and temperature specified in Table 4. During immersion, the radius of bend of the
specimens shall be not less than 14, nor more than 35, times the specified maximum diameter
of the wire or cable under test. Upon removal from the fluids, the specimens shall remain for 1
hour in free air at room temperature. The diameters shall then be remeasured at the original
point of measurement and compared to the initial diameters. The percent change in diameter
shall then be calculated. For finished wire, 1 inch (25 mm) of insulation shall be removed from
each end of a 24-inch (610-mm) length of each specimen. For finished cable, 2 inches (51 mm)
of the jacket shall be removed from each end of a 24-inch (610-mm) length of each specimen,
and the shield shall be pushed back and formed into a pigtail at each end of the specimen. One
inch (25 mm) of insulation of each of the primary wires shall then be removed from each end
of the specimen. The specimens shall then be subjected to the bend test (4.6.1 - use the
mandrels and test weights specified on the applicable specification sheet for the Crosslinking
Proof Test), followed by the voltage withstand test (4.6.14).
TABLE 4
IMMERSION TEST FLUIDS
TEST FLUID
TEST TEMPERATURE IMMERSION
TIME
(a) MIL-L-23699, Lubricating Oil, Aircraft Turbine
Engine,Synthetic Base 48 to 50°C (118 to 122°F) 20 hours
(b) MIL-H-5606, Hydraulic Fluid, Petroleum Base,
Aircraft, Missile and Ordnance 48 to 50°C (118 to 122°F) 20 hours
(c) TT-I-735, Isopropyl Alcohol 20 to 25°C (68 to 77°F) 168 hours
(d) MIL-T-5624, Turbine Fuel, Aviation, Grade JP-4
or JP-8 20 to 25°C (68 to 77°F) 168 hours
(e) SAE-AS-1241, Fire Resistant Phosphate Ester
Hydraulic Fluid for Aircraft 48 to 50°C (118 to 122°F) 20 hours
(f) MIL-L-7808, Lubricating Oil, Aircraft Turbine
Engine, Synthetic Base; or NATO 148 118 to 121°C (244 to 250°F)
30 minutes
4.6.9 Insulation Elongation and Tensile Strength
Specimens of the entire insulation shall be carefully removed from the conductor and tested for
tensile strength and elongation in accordance with FED-STD-228, Methods 3021 and 3031,
respectively, using 1-inch (25-mm) bench marks, a 1-inch (25-mm) initial jaw separation, and a
jaw separation speed of 2 inches (51 mm) per minute. For cables, the method shall be the same,
but only the cable jacket shall be tested.
4.6.10 Jacket Concentricity
The concentricity of the cable jacket shall be determined by first locating and recording the
minimum wall thickness measured on a cross-section of the jacket. The maximum wall thick-
ness of this same cross-section of the jacket shall also be measured and recorded. The ratio of
the minimum wall thickness to the maximum wall thickness shall define the concentricity. All
wall-thickness measurements shall be made under suitable magnification. The wall thickness
shall be the radial distance between the inner and outer rim of the jacket.